degree of freedom energy equations virtual...
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Degree of FreedomEnergy EquationsVirtual Work
k (N/m) c (Ns/m)
Static Equilibrium Position
kmg
static =δ
f(t)
x(t)
m
F(t) input
X(t) output
1 DOF System (Mass&Spring)
MECHANICAL SYSTEMS
k (N/m)
f(t)
m
x(t)c (Ns/m)
21 2
1 xmE &=
22 2
1 kxE =
xxcxtfW δ−δ=δ &)(
Lagrange’s Equation:
ixii
QxE
xE
dtd
=∂∂
+⎟⎟⎠
⎞⎜⎜⎝
⎛∂∂ 21&
Lagrange’s equation is written for linear systems as follow
Where xi is the ith generalized co-ordinate and Qxi is the generalizedforce subjected to the ith generalized co-ordinate.
ixii
Qx
EEx
EEdtd
=∂−∂
−⎟⎟⎠
⎞⎜⎜⎝
⎛∂−∂ )()( 2121&
For Mass&spring system, application of the Lagrange’s equation givesthe “Equation of Motion”.
( ) xmxmdtd
xE
dtd
&&&&
==⎟⎠⎞
⎜⎝⎛∂∂ 1
kxx
E=
∂∂ 2
xctfQx &−= )(
xctfkxxm &&& −=+ )(
)(tfkxxcxm =++ &&&
Viscous damping, B (Nms/rad)
R
k
c
221 mRI =
m M(t)
θ
RθR Sinθ
For θ<<1
Sin(θ)=θ
Cos(θ)=1
21 2
1θ= &IE
22 )(
21
θ= RkE
)R(cRB)t(MW θδθ−δθθ−δθ=δ &&
≈R
221 2
121
θ= &mRE
222 2
1θ= kRE 1 DOF system, θ
Lagrange’s equation for θ
θ=⎟⎠⎞
⎜⎝⎛ θ=⎟
⎠⎞
⎜⎝⎛
θ∂∂ &&&&
22121
21 mRmR
dtdE
dtd θ=
θ∂∂ 22 kRE
θ−θ−=θ&& 2cRB)t(MQ
( ) )t(MkRcRBmR21 222 =θ+θ++θ &&&
)R(cRB)t(MW θδθ−δθθ−δθ=δ &&
1 DOF system, θL
kc
θF(t)
L/4 3L/8 3L/8
GA B
D
21 2
1θ= &BIE
Homogeneous beam is pinned at point B. The moment of inertia with respect to point B is calculated from theSteiner Theorem.
2mrII GB +=
r
442LLLr =−=
22
4121
⎟⎠⎞
⎜⎝⎛+=
LmmLIB
C
22
4121
⎟⎠⎞
⎜⎝⎛+=
LmmLIB 487
483
484
16121 2222
2 mLmLmLLmmLIB =+=+=
2221 48
721
21
θ=θ= && mLIE B 1621
421)(
21 222
22
θ=⎟
⎠⎞
⎜⎝⎛ θ==
LkLkxkE A
DDC xxcxtFW δ−δ=δ &)( θ=θ=8
6,8
3 LxLx DC
⎟⎠⎞
⎜⎝⎛ θδθ−⎟
⎠⎞
⎜⎝⎛ θδ=δ
86
86
83)( LLcLtFW & δθθ−δθ−=δ &
6436
83)(
2LcLtFW
δθ⎟⎟⎠
⎞⎜⎜⎝
⎛θ−−=δ &
6436
83)(
2LcLtFW
Lagrange’s equation for θ
2221 48
721
21
θ=θ= && mLIE B 1621
421)(
21 222
22
θ=⎟
⎠⎞
⎜⎝⎛ θ==
LkLkxkE A
δθ⎟⎟⎠
⎞⎜⎜⎝
⎛θ−−=δ &
6436
83)(
2LcLtFW
θ=⎟⎠⎞
⎜⎝⎛ θ=⎟
⎠⎞
⎜⎝⎛
θ∂∂ &&&&
221487
487 mLmL
dtdE
dtd
θ=θ∂
∂16
22 LkE
θ−=θ&
169)(
83 2cLtFLQ
)(161
169
487
83222 tFkLcLmL L−=θ+θ+θ &&&
ELECTRICAL SYSTEMS
L R
V1C V2
q&
L-R-C Circuit
L
q&
dtqdLVV ba&
=−
a b
(Henry)
R
q&
(Ohm)
a b
qRVV ba &=−
b
q&a C
(Farad)
qC
VV ba1
=−
According to the Kirschhoff’s Rule,
2111 VqC
andVqC
qRdtqdL ==++ &&
Where V1 denotes the input voltage and V2 denotes the output voltage.
The energy and virtual work equations for L-R-C circuit are
21 2
1 qLE &= 22 2
1 qC
E = qqRqVW δ−δ=δ &1
There is only one current in the circuit and then the system is said to be 1 DOF. The generalized co-ordinate is the charge q.
Application of the Lagrange’s equation to charge q establishes themathematical model.
( ) qLqLdtd
qE
dtd
&&&&
==⎟⎟⎠
⎞⎜⎜⎝
⎛∂∂ 1
21 2
1 qLE &= 22 2
1 qC
E = qqRqVW δ−δ=δ &1
qCq
E 12 =∂∂ qRVQq &−= 1
11 VqC
qRqL =++ &&& 21 VqC
and =
Laplace Transformation (Kuo, 1995)
The Laplace transform is one of the mathematical tools used for thesolution of linear ordinary differential equations. In comparison with theclassical method of solving linear differential equations, the Laplacetransform method has the following two attractive features:
1.The homogeneous equation and the particular integral of the solutionare obtained in one operation.
2.The Laplace transform converts the differential equation into an algebraic equation in s. It is then possible to manipulate the algebraicequation by simple algebraic rules to obtain the solution in the s-domain. The final solution is obtained by taking the inverse Laplacetransform.
Definition of the Laplace Transform
Given the real function f(t) that satisfies the condition
∫∞ σ− ∞<0
)( dtetf t
For some finite real σ, the Laplace transform of f(t) is defined as
∫∞ −=0
)()( dtetfsF st
The variable s is referred to as the Laplace operator which is a complex variable; that is,
ω+σ= is
Example 1.
Let f(t) be a unit-step function that is defined as
⎩⎨⎧
<>=
0001)(
)(tttu
tf
The Laplace transform of f(t) is obtained as
[ ]s
es
dtetutuLsF stst 11)()()(00=−===
∞−∞ −∫
Example 2.
Consider the exponential function
tetf α−=)(
where α is a real constant
α+=−==
∞α+−
∫∞
α+−α−
sdteesF s
estt ts 1)(0
)(
0
Important Theorems of the Laplace Transform
Theorem 1: Multiplication by a Constant
Let k be a constant and F(s) be the Laplace transform of f(t). Then
[ ] )()( skFtkfL =Theorem 2: Sum and Difference
Let F1(s) and F2(s) be the Laplace transform of f1(t) and f2(t), respectively. Then
[ ] )()()()( 2121 sFsFtftfL ±=±Theorem 3: Differentiation
)0()()(lim)()(0
fssFtfssFdt
tdfLt
−=−=⎥⎦⎤
⎢⎣⎡
→
)0(...)0()0()()( )1(21 −−− −−′−−=⎥⎥⎦
⎤
⎢⎢⎣
⎡ nnnnn
ffsfssFsdt
tfdL
Theorem 4: Integration
ssFdfL
t )()(0
=⎥⎦⎤
⎢⎣⎡ ττ∫
Theorem 5: Initial -Value Theorem
)(lim)(lim0
ssFtfst ∞→→
=
Theorem 6: Final -Value Theorem
)(lim)(lim0
ssFtfst →∞→
=
)(tfkxxcxm =++ &&&
Apply the Laplace transform to the equation of motion of the mass-springsystem
[ ] [ ] )()()0()()0()0()(2 sFskXxssXcxsxsXsm =+−+−− &
[ ] ( ) )()0()0(1)(2 sFxxssXkcsms =−+−++ &
[ ] )()(2 sFsXkcsms =++
kcsmssFsXsH
++== 2
1)()()(
kcsms ++21F(s) X(s)
)(1)( 2 sFkcsms
sX++
=
(Transfer Function)
All initial conditions are assumed to be zero while evaluating the Transfer Function.
k (N/m)
f(t)
m
x(t)c (Ns/m)
m=200 kgc=300 Ns/mk=5000 N/m
f(t)=50 N (step function)
t (sec)
f(t)
50
ssF 50)( =
MATLAB Code
clc;clear;
m=200;
c=300;
k=5000;
pay=[1];
payda=[m,c,k];
step(pay*50,payda)
skcsmssX 501)( 2 ++=
0 1 2 3 4 5 6 7 80
0.002
0.004
0.006
0.008
0.01
0.012
0.014
0.016
0.018Step Response
Time (sec)
Ampl
itude
Steady-state value
x(t)
msss
sssXtxxst
ss 01.050005050
50003002001)(lim)(lim 20
==++
===→∞→